Refractory metal ceramics and methods of making thereof

ABSTRACT

A composition having nanoparticles of a refractory-metal carbide or refractory-metal nitride and a carbonaceous matrix. The composition is not in the form of a powder. A composition comprising a metal component and an organic component. The metal component is nanoparticles or particles of a refractory metal or a refractory-metal compound capable of decomposing into refractory metal nanoparticles. The organic component is an organic compound having a char yield of at least 60% by weight or a thermoset made from the organic compound. A method of combining particles of a refractory metal or a refractory-metal compound capable of reacting or decomposing into refractory-metal nanoparticles with an organic compound having a char yield of at least 60% by weight to form a precursor mixture.

This application is a divisional application of U.S. Pat. No. 9,403,723,issued on Aug. 2, 2016, which is a divisional application of pendingU.S. Pat. No. 8,822,023 issued on Sep. 2, 2014, which claims the benefitof U.S. Provisional Application No. 61/590,852, filed on Jan. 26, 2012,U.S. Provisional Application No. 61/640,744, filed on May 1, 2012, U.S.Provisional Application No. 61/669,201, filed on Jul. 9, 2012, and U.S.Provisional Application No. 61/693,930, filed on Aug. 28, 2012. Theprovisional applications and all other publications and patent documentsreferred to throughout this nonprovisional application are incorporatedherein by reference.

TECHNICAL FIELD

The present disclosure is generally related to synthesis of refractorymetal ceramics, such as titanium carbide and titanium nitride.

DESCRIPTION OF RELATED ART

Refractory transition metal carbides (MC) and nitrides have the highestknown melting points (2600-3900° C.) and also outstanding hardness,chemical inertness, wear resistance, electrocatalytic activity, andneutron absorption ability. Films, fibers, and powders of these ceramicshave been made from polymeric precursors, but large monolithic shapeselude the polymeric method. Refractory MCs are typically prepared bypowder metallurgy methods such as hot press sintering. Ordinarily, metalcarbide ceramics made by these techniques, which are both energy andtime intensive, result in brittle materials, owing partly to the largegranular structure and the inconsistency in the MC particle sizes.Powdered metal nitrides can be produced from metal particles in a flowof nitrogen but have to be formulated into shaped components underpressure and high temperatures.

Since the late 1960s, there has been an interest in high temperatureceramic materials for such applications as grinding/machining, ballbearings, armors, fibers, and turbine blades but structural applicationshave been lacking due to their brittleness and weakness in shear andtension. More recently, there has been a resurgence of interest inultra-high temperature materials for hypersonic vehicles (Mach 5-20)with new propulsion and structural concepts. These vehicles includeballistic missiles, hypersonic cruise missiles, re-entry vehicles, spaceaccess vehicles, interceptor missiles, and hypersonic cruise aircraft,which can be easily divided into single-use expendable and reusablesystems. These expendable and reusable space vehicles, next generationrocket engines, and hypersonic spacecraft need tough materials andstructural components capable of operating at temperatures in excess of2200° C. and must meet several requirements simultaneously, such as highmelting temperature, high strength, and environmental resistance(oxidative resistance). A hypersonic commercial aircraft would be ableto travel from New York to Los Angeles in less than an hour. Thus,current increasing interest in hypersonic vehicles and weapons points tothe need for new ultra-high temperature materials for wing leading edgesand nose tips along with propulsion system components.

For these applications, progress will come when materials are developedthat can be easily processed into shaped components with the requiredthermomechanical and thermochemical characteristics and properties andthat can perform without some form of cooling at temperatures exceeding2200° C. Such materials do not currently exist. The refractoryinterstitial transition metal carbides are extremely hard, inert, andrefractory materials. Unfortunately, they are also brittle and difficultto machine.

There is current interest in metal carbides with small particle size andhigh surface area such as tungsten carbide (WC) due to their potentialapplication as catalysts. Selected MCs such as WC with outstandingcatalytic properties similar to Pt promise to be an inexpensivealternative to the expensive noble metals such as Pt and Pd withpossibly even superior properties due to their ability to withstand hightemperatures and resistance to poisoning, which is common with the noblemetals. The anodic chemistry of the direct methanol fuel cell (DMFC)requires the oxidation of methanol and the decomposition of water toproduce protons, electrons, and CO₂. Strong chemisorption of CO on thenoble metals makes these electrocatalysts susceptible to CO poisoning,blocking the active site for methanol oxidation. Consequently, thediscovery of less expensive catalysts such as WC, which is more COtolerant, has helped to commercialize the DMFC.

BRIEF SUMMARY

Disclosed herein is a composition comprising nanoparticles of arefractory-metal carbide or refractory-metal nitride and a carbonaceousmatrix. The composition is not in the form of a powder.

Also disclosed herein is a composition comprising a metal component andan organic component. The metal component is selected from nanoparticlesor particles of a refractory metal and a refractory-metal compoundcapable of decomposing into refractory-metal nanoparticles. The organiccomponent is selected from an organic compound having a char yield of atleast 60% by weight and a thermoset made from the organic compound.

Also disclosed herein is a method comprising combining particles of arefractory metal or a refractory-metal compound capable of reacting ordecomposing into refractory-metal nanoparticles with an organic compoundhaving a char yield of at least 60% by weight to form a precursormixture.

Also disclosed herein is a method comprising: providing a precursormixture of particles of a refractory metal or a refractory-metalcompound capable of decomposing into refractory-metal nanoparticles andan organic compound; heating the precursor mixture in an inertatmosphere at elevated pressure and at a temperature that causesdecomposition of the refractory-metal compound to form refractory-metalnanoparticles to form a metal nanoparticle composition; and heating themetal nanoparticle composition in an inert atmosphere, argon, ornitrogen at a temperature that causes formation of a ceramic comprisingnanoparticles of a refractory-metal carbide or a refractory-metalnitride in a carbonaceous matrix. The organic compound has a char yieldof at least 60% by weight when heated at the elevated pressure.

BRIEF DESCRIPTION OF THE DRAWINGS

A more complete appreciation will be readily obtained by reference tothe following Description of the Example Embodiments and theaccompanying drawings.

FIG. 1 schematically illustrates a process for forming the disclosedcompositions.

FIG. 2 schematically illustrates metal nanoparticles 10 embedded in athermoset matrix 20.

FIG. 3 schematically illustrates the transfer 40 of carbon atoms fromthe carbon matrix 30 to the nanoparticles 50.

FIG. 4 schematically illustrates metal carbide nanoparticles 60 in acarbonaceous matrix 70.

FIG. 5 shows an X-ray diffraction analysis (XRD) of a sample containingTiC nanoparticles.

FIG. 6 shows an XRD of a sample containing TiN nanoparticles.

FIG. 7 shows an XRD of a sample containing ZrC nanoparticles.

FIG. 8 shows an XRD of a sample containing ZrN nanoparticles.

FIG. 9 shows an XRD of a sample containing HfC nanoparticles.

FIG. 10 shows an XRD of a sample containing TiC nanoparticles afterheating to 1600° C.

FIG. 11 shows a scanning electron micrograph (SEM) of a samplecontaining TiC nanoparticles.

FIG. 12 shows an XRD of a sample containing WC nanoparticles.

FIG. 13 shows an SEM of a sample containing WC nanoparticles.

DETAILED DESCRIPTION OF EXAMPLE EMBODIMENTS

In the following description, for purposes of explanation and notlimitation, specific details are set forth in order to provide athorough understanding of the present disclosure. However, it will beapparent to one skilled in the art that the present subject matter maybe practiced in other embodiments that depart from these specificdetails. In other instances, detailed descriptions of well-known methodsand devices are omitted so as to not obscure the present disclosure withunnecessary detail. Any numerical range disclosed herein includes everynumber within the range as well as those within rounding error of theend point of the range.

Disclosed herein is (1) a method for the in situ formation of refractorymetal carbide (Groups IV-VI) ceramics with or without a carbon matrix inone step affording a shaped composition with structural integrity, (2)various refractory metal nanoparticle-precursor/thermoset compositionsand metal-carbide and metal carbide-carbon matrix compositions atmultiple stages, (3) the nanoparticle metal-carbide and nanoparticlemetal carbide-carbon matrix compositions, (4) nanoparticle metalnitride-carbon matrix compositions, (5) fiber reinforced metal-carbideand metal carbide-carbon matrix composites, and (6) fiber reinforcedmetal nitride-carbon matrix composites.

The methods may produce refractory metal (Ti, W, Nb, Zr, Mo, Cr, V, Ta,and Hf) carbides and nitrides in shaped solid configurations from metalnanoparticles. Mixed phases can also be produced. The ceramics areproduced as nanoparticles. When a) any metal compound that decomposesinto highly reactive metal nanoparticles is combined with b) carbonprecursors that melt and only contain carbon and hydrogen, thecombination may be thermally converted to c) a solid shape containinghigh yields of pure metal carbides and/or metal nitrides. Theappropriate metal nanoparticles are formed in situ from the thermaldecompositions of metal carbonyls and metal hydrides within the melt ofthe carbon precursor. The carbon sources may be melt processablearomatic-containing acetylenes or low molecular weight polymers thatexhibit extremely high char yields. The carbon precursor may containonly C and H to insure that heteroatoms are not incorporated into theinterstitial sites of the metal nanoparticles during the reaction toproduce the metal carbide and/or metal nitride. The metal carbides ormetal nitrides may form between 600-1000° C. under inert conditions fromreaction of the highly reactive metal nanoparticles with either thecarbon precursor (degradation above 500° C.) or nitrogen gas,respectively, but in some cases the reaction can be made to occur fasterat higher temperatures. The temperatures at which the synthetic processoccurs may be well below those normally associated with the formation ofcarbide and nitride ceramics. When an excess of the carbon precursor isused, the individual formed ceramic particles may be glued or boundtogether with the resulting nanostructured or amorphous elastic carbonto afford structural integrity.

In the methods disclosed herein (FIG. 1), metal compounds are combinedwith a carbon precursor. The carbon precursors are compounds such aspolymers or resins with functional unsaturation to interact with themetal nanoparticles that form from the metal compounds. Theunsaturations also permit the carbon precursor to undergo conversionfrom the melt to form thermosets or crosslinked polymers. A typicalcomposition includes the carbon precursor and the metal compound ormultiple metal compounds. Upon heating this composition, the carbonprecursor melts at its melting point and may be thermally converted to ashaped solid thermoset 20 through reaction of the unsaturated sites. Itis possible that during this step or a subsequent step the metalcompound thermally decomposes into metal nanoparticles 10 or the metalpowder reacts with the organic component to form nanoparticles which areembedded in the solid thermoset (FIG. 2). Alternatively, the formationof the metal nanoparticles may occur later during the next step in theprocess, which is extended heat treatment at higher temperatures.Thermal treatment of the thermoset above 500° C. results incarbonization of the carbon precursor 30 yielding carbon atoms thatreact 40 in an argon atmosphere with the interstitial sites of the metalnanoparticles 50 affording the metal carbides 60, which are embedded inthe excess carbon 70 (FIGS. 3-4). When the same reaction is performed ina flow of nitrogen or when the organic compound contains nitrogen, metalnitride-carbon matrix compositions are also formed in a stoichiometricratio. Depending on the shape and thickness of the composition, bothmetal nitride and metal carbide may form with the metal carbide on theinterior part of composition where the nitrogen cannot be in intimatecontact.

Reaction of metal salts and decomposition to metal nanoparticles mayoccur at lower temperatures with reaction to the ceramics occurring by1200° C. but higher temperatures may be needed at least to 1600° C. formetal powders of micron size. Smaller size particles may react fasterand be totally consumed at lower temperatures relative to the largerparticle size powders. The particle size of the metal carbide/nitridecan be controlled as a function of the upper temperature treatment withhigher exposure temperatures affording larger particle size ceramics.

Regardless of the ratio of metal compound to carbon source, the metalcarbides or nitrides may form as nanoparticles. This is a highlydesirable result, as it is generally accepted that homogeneousnanoparticle composites of ceramics will have better properties thantheir much more common microparticle counterparts. An excess of carbonatoms can be made available for reaction with the metal content and toensure the formation of a carbon matrix in which the refractory metalcarbides are bound, or the reaction can be conducted stoichiometricallyto yield only the metal carbide. The amount of metal carbide and carbonwithin the resulting composition can be varied based on the quantity ofeach individual component (metal compound and melt processable carboncompound) mixed for usage in the precursor composition. When thereaction is performed in a nitrogen atmosphere, the metal nanoparticlemay preferentially react with the nitrogen relative to the carbonaffording the corresponding metal nitrides in pure form.

Carbon, ceramic, and metal fibers may be incorporated into variousmixtures of precursor compositions composed of metal compounds of GroupsIV-VI and the acetylene-containing aromatic compounds or polymers(carbon source) and the resulting fiber-containing mixture is convertedto a shaped solid at temperatures below 500° C. followed by heating totemperatures around 1000-1200° C. yielding a fiber reinforced metalcarbide-carbon matrix composite. The precursor composition (metal saltand carbon precursor) described above are mixed with continuous fibersor chopped fibers and heated until conversion to the shaped thermosetforms. Further heating above 500° C. in an inert atmosphere (argon)results in the formation of the fiber reinforced refractory metalcarbide-carbon matrix composites. Depending on the ceramic being formed,the tough, solid shaped composite can be used for structuralapplications in excess of 3000° C. The composite may be exposed to anupper temperature for which it is going to be used so that the physicalproperties may remain intact and not change. The precursor compositioncan contain a combination of different refractory metal compounds thatwill lead to a mixture of ceramics in the composite, which could bebeneficial for specific applications.

As noted above, when the metal compound and carbon precursor compositionare heated in a nitrogen atmosphere, metal nitride ceramics may formwith a direct incorporation of nitrogen into the lattices of the metalatoms/nanoparticles. Thus, by changing the atmosphere for performing thereaction, one can selectively form either the metal-carbidecarbon-matrix composition or the metal-nitride carbon-matrix compositionor combination thereof. When the fiber experiments are carried out in anitrogen atmosphere, fiber reinforced refractory metal nitride-carbonmatrix composites will be formed especially on the outer surface. Thecomposite may have outstanding oxidative stability and temperaturecapabilities in excess of 3000° C.

The process is outlined in FIG. 1 and schematically illustrated in FIGS.2-4. Any reactions described are not limiting of the presently claimedmethods and compositions. It is speculated that the nanoparticle form ofthe refractory metal activates its reaction with the carbon source,thereby lowering the temperature of metal carbide or metal nitrideformation. Moreover, by varying the amount of metal compound that formsreactive metal nanoparticles relative to the carbon precursor, theamount of metal carbide or metal nitride can be changed with respect tothe amount of carbon matrix in order to vary the properties of theresulting composite. The metal carbide or metal nitride carbon-matrixcomposites are expected to show enhanced toughness, owing to thepresence of the relatively elastic carbon, which would exist in formsranging from amorphous to nanotube to graphitic carbon.

The native presence of an “elastic” carbon matrix may allow fortoughening of the inherently brittle sintered ceramics. The carbon maypermit operation of the toughened ceramic at extremely hightemperatures, owing to carbon's high melting point (>3000° C.).Ceramic/carbon-matrix compositions are currently sought for thesereasons, and the present method may permit straightforward preparationof these composites in a single step for the first time, in contrast tothe traditional means of first forming the ceramic powder and thenpreparing the carbon-matrix composite under sintering conditions. Also,the ratio of ceramic to carbon is easily tuned based only on the ratioof metal-compound or metal powder to carbon-precursor.

Fiber-reinforced refractory metal carbide and metal nitride carbonmatrix composites may exhibit outstanding mechanical properties forusage under extreme environmental high temperature conditions. Finelydivided fiber reinforced refractory metal carbide carbon composites canallow the consolidation of fully dense shaped solid components withextreme fracture resistance for uses in high stress and temperatureapplications such as advanced engine components for hypersonic vehiclesand automobiles, where increased operation temperature and mechanicalintegrity could translate into tremendous economic advantages. Suchtough, easily shaped ceramic composites are critical to the nextgeneration of jet engines, which are being designed to operate at higherinternal temperatures and stresses than those in current service, and inadvanced automobile engines and supporting components. High temperatureship deck plates could be readily fabricated for aircraft carriersneeding the superior heat resistant properties of the metal carbideand/or metal nitride ceramic-carbon composites. Also, lightweight,tough, and hard ceramics easily made in controllable forms could be veryimportant for the fabrication of superior military armor; againfabricated in a mold in a shaped structure. Tungsten carbide (WC) iscurrently used as warheads for munitions due to its superior hardnessand high density and would be more economical to produce by the WCformulated from the precursor compositions disclosed herein. The abilityto fabricate tough, shaped refractory metal carbide or metal nitridecomponents in one step enhances their importance due to the economicadvantages and the elimination of machining to a shaped component.

In the first step of the method, two components are combined and may bethoroughly mixed. One is a metal component which may be arefractory-metal compound capable of decomposing into refractory metalnanoparticles or particles of a refractory metal. Any refractory metalmay be used, including but not limited to a group IV-VI transitionmetal, titanium, zirconium, hafnium, tungsten, niobium, molybdenum,chromium, tantalum, or vanadium. When a pure metal is used, it may be inthe form of nanoparticles or other particles such as a powder. When suchmetal particles are used, the metal may directly react with the organiccomponent. Suitable powders include, but are not limited to, tungstenand tantalum.

Instead of pure metal, a compound containing the metal atom may be used.Such compounds decompose at elevated temperatures, releasing the metalatoms so that they may react with the organic component. Suitable suchcompounds include, but are not limited to, a salt, a hydride, a carbonylcompound, or a halide of the refractory metal. Examples include titaniumhydride, zirconium hydride, and hafnium hydride. Other examples andembodiments of types of compounds which may be used with the metalsdisclosed herein may be disclosed in U.S. Pat. Nos. 6,673,953;6,770,583; 6,846,345; 6,884,861; 7,722,851; 7,819,938; 8,277,534.

The other component is an organic compound that has a char yield of atleast 60% by weight. The char yield may also be as high as at least 70%,80%, 90%, or 95% by weight. The char yield of a potential compound maybe determined by comparing the weight of a sample before and afterheating to at least 1000° C. for at least 1 hr in an inert atmospheresuch as nitrogen or argon. Any such compounds with high char yields maybe used as the charring may play a role in the mechanism of thereactions. This char yield may be measured at an elevated pressure to beused when a heating step is also performed at such pressure. Thus, acompound having a low char yield at atmospheric pressure but having ahigh char yield under the conditions that the disclosed methods areperformed may be suitable.

Certain organic compounds may exhibit any of the followingcharacteristics, including mutually consistent combinations ofcharacteristics: containing only carbon and hydrogen; containingaromatic and acetylene groups; containing only carbon, hydrogen, andnitrogen or oxygen; containing no oxygen; and containing a heteroatomother than oxygen. It may have a melting point of at most 400° C., 350°C., 300° C., 250° C., 200° C. or 150° C. and the melting may occurbefore polymerization or degradation of the compound. Examples oforganic compounds include, but are not limited to,1,2,4,5-tetrakis(phenylethynyl)benzene (TPEB), N,N′-(1,4-phenylenedimethylidyne)-bis-(3-ethynylaniline) (PDEA),N,N′-(1,4-phenylenedimethylidyne)-bis(3,4-dicyanoaniline)(dianilphthalonitrile), and 1,3-bis(3,4-dicyanophenoxy)benzene(resorcinol phthalonitrile). Prepolymers may also be used, such as aprepolymer of TPEB or other suitable organic compounds. Differentcompounds can be blended together and/or reacted to a prepolymer stagebefore usage as the organic compound of the precursor composition. Thepresence of nitrogen atoms in the organic compound may produce metalnitrides in the ceramic without the use of a nitrogen atmosphere.

More than one metal, metal compound, and/or organic compound may beused. Two or more different metals may be used to produce two differentmetal carbides and/or nitrides in the ceramic. Also, in some cases onlyone compound may be used when the metal component and the organiccomponent are the same compound. Such compounds may be high in carbonand hydrogen to produce a high char yield, but also have a refractorymetal bound to the compound.

An optional third component in the precursor materials is a plurality offibers or other fillers. Examples of fibers include, but are not limitedto, carbon fibers, ceramic fibers, and metal fibers. The fibers may beof any dimension that can be incorporated into the mixture and may becut or chopped to shorter dimensions.

The precursor mixture, which may be mixed in a melt stage, thenundergoes a heating step to form a metal nanoparticle composition. Thismay be performed while the mixture is in a mold. This will allow thefinal product to have the same shape as the mold, as the mixture willmelt if not already liquid and fill the mold during the heating, andretain its shape when the ceramic is formed. The precursor mixture isheated in an inert atmosphere at a temperature that causes decompositionof the refractory-metal compound to form refractory-metal nanoparticles.If the organic compound is volatile, the heating may be performed underpressure to avoid evaporation of the organic compound. As used herein,this heating step includes the formation of nanoparticles from a metalpowder. As the reaction proceeds from the metal powder, the metalparticles will become smaller. It is not necessary to verify that thenanoparticles are formed in order to continue with the method. However,any known technique for detecting nanoparticles such as SEM or x-raydiffraction analysis (XRD) may be used if desired to verify that themetal component suitably produces nanoparticles. Suitable heatingtemperatures include, but are not limited to, 150-500 or 600° C.

Heating the precursor may also cause the polymerization of the organiccompound to a thermoset. The metal nanoparticles 10 would then bedispersed throughout the thermoset 20 as shown in FIG. 2. The organiccompound may also polymerize before the nanoparticles are formed. Athermoset having the refractory-metal compound or particles (includingnanoparticles) of refractory metal dispersed throughout may be used as afinal product. The thermoset may also be machined to a desired shape,followed by heating to form a ceramic as described below.

The metal source may be homogeneously distributed or embedded in thethermoset as an intermediate shaped solid. At this stage, thecomposition may have a shape that it will retain upon further heatingand conversion to the ceramic from reaction of the metal source with thedeveloping carbon matrix.

The precursor mixture may be consolidated to a shaped solid componentunder pressure to promote intimate contact of the reactants to provide avery dense ceramic solid or to densify the final product. The precursormixture may be compacted under exterior pressure, removed from thepressure, and then heated to a thermoset followed by conversion to theceramic. Alternatively, the precursor mixture may be compacted underexterior pressure and the pressure maintained while heating to thethermoset and ceramic.

In a second heating step, the metal nanoparticle composition is heatedto form a ceramic. The heating is performed at a temperature that causesformation of nanoparticles of a refractory-metal carbide or arefractory-metal nitride 60 in a carbonaceous matrix 70 (FIG. 4). Thecarbonaceous matrix may comprise graphitic carbon, carbon nanotubes,and/or amorphous carbon. If an inert atmosphere such as argon is used,metal carbide nanoparticles may be formed. If nitrogen is present, metalnitride nanoparticles may be formed. There may be a higher concentrationof nitrides on the surface than in the interior. Suitable heatingtemperatures include, but are not limited to, 500-1900° C.

Nanoparticles that may be formed include, but are not limited to,titanium carbide, titanium nitride, zirconium carbide, zirconiumnitride, hafnium carbide, hafnium nitride, tungsten carbide, tungstennitride, tantalum carbide, and tantalum nitride. The presence andcomposition of the metal carbide or nitride particles may be verified byany known technique for detecting nanoparticles such as SEM or XRD. Thenanoparticles may have an average diameter of less than 100 nm, 50 nm,or 30 nm. They may be generally spherical in shape or may benon-spherical, such as nanorods.

The ceramic may include any amount of nanoparticles, including but notlimited to, at least 5%, 10%, 20%, 30%, 40%, 50%, 60%, 70%, 80%, 90%,95%, or 99% by weight of nanoparticles. The percentage of nanoparticlesmay be in part determined by the molar ratio of metal to carbon atoms inthe precursor mixture. At a 1:1 ratio, nearly all of the carbon may beincorporated into the nanoparticle, leaving a small amount or trace ofcarbonaceous matrix. With higher amounts of organic compound, thefraction of nanoparticles is lower and the fraction of carbonaceousmatrix is higher. By this method, variations in the ratio of metal toorganic may be used, affording a mixture of metal carbide when performedin an inert atmosphere such as argon and metal nitride when performed ina nitrogen atmosphere. When metal nitrides are made, raising the amountof carbon in the precursor mixture may lower the amount of metal nitridein the ceramic.

The ceramic is not formed as a powder and may be in the form of a solid,unbroken mass. It may contain less than 20% by volume of voids or as lowas 10%, 5%, or 1%. A WC-carbon ceramic may be made with less than 50%voids. It may have the same shape as the precursor mixture or it maytake on the shape of a mold it was placed in during the heating. Theceramic may retain its shape in that it does not crumble when handledand may not change shape or break without the use of extreme force. Theceramic composition may be tough, hard, and have structural integrity.The degree of such properties may depend on the amount of ceramic tocarbon in the solid ceramic solid composition. Any shape may be formedto make an article useful for incorporation into an apparatus. Thearticle may be large enough to have a minimum size of at least 1 cm inall dimensions. That is, the entire surface of the article is at least 5mm from the center of mass of the article. Larger articles may be made,such as having a minimum size of at least 10 cm in all dimensions. Also,the composition may have smaller sizes, such as 1 mm, 2 mm, or 5 mm.

A third heating step may also be performed, where the ceramic is heatedin an oxygen-containing atmosphere to form an oxide of the refractorymetal on the surface of the ceramic. For example, titanium oxide may beformed on the surface. Such surface oxidation may protect the interiorof the ceramic from further oxidation.

The following examples are given to illustrate specific applications.These specific examples are not intended to limit the scope of thedisclosure in this application. Any other appropriate methods andmaterials disclosed in U.S. Provisional Application Nos. 61/590,852;61/640,744; 61/669,201; 61/693,930 may be used. Any carbon source, metalcompound, and/or other parameter disclosed therein may be used in anycombination in the presently disclosed method, and may be combined withany material and/or parameter disclosed in the present application.

Example 1

Formulation of Precursor Composition of TiH₂ and TPEB—

TPEB (0.1016 g; 0.2125 mmol) and TiH₂ (0.2008 g; 4.0224 mmol) werethoroughly mixed and used as the precursor composition for the formationof refractory nanoparticle TiC embedded or bonded with the excess ofcarbon that behaves as a matrix material. The ratio of the two reactantscan be readily varied by the described formulation method.

Example 2

Formation of Refractory TiC Solid Ceramic in One Step by Heating at 10°C./Min to 1400° C. Under an Argon Atmosphere—

A sample (5.8911 mg) of the precursor composition prepared in Example 1was weighed into a TGA ceramic pan and directly heated at 10° C. under aflow (100 cc/min) of argon to 1400° C. yielding a solid ceramic materialwith a weight retention of 89.24%. During the heat treatment, the samplemelted at about 194° C. (endothermic transition; TPEB) and exhibited anexothermic transition peaking at about 292° C. (cure to thermoset solidpolymer). The solid ceramic was removed from the TGA pan andcharacterized by XRD and was found to have formed nanoparticle sized TiCin an excess of carbon as the matrix. The TiC carbon solid compositionwas formed in one step and exhibited structural integrity. FIG. 5 showsa typical XRD of a TiC sample made by the method of this example.

Example 3

Formation of Refractory TiC Solid Ceramic in One Step by ControlledHeating to 1200° C. Under an Argon Atmosphere—

A sample (62.1426 mg) of the precursor composition prepared in Example 1was heated under an argon atmosphere at 5° C./min to 250° C. and held atthis temperature for 2 hr to consolidate to a solid shaped thermosetpolymer. During the heat treatment to 250° C., the sample showed anendothermic transition at about 195° C. attributed to the melting pointof TPEB. The isothermal heat treatment at 250° C. resulted in thereaction of the ethynyl units in the TPEB and conversion to the shapedthermoset polymer. The solid polymeric sample composed of TiH₂ and thepolymeric thermoset was slowly heated at 1° C./min to 1200° C. and heldat this temperature for 6 hr affording a weight retention of 89.78%.Above 400° C., degradation of the TiH₂ occurred to Ti nanoparticles andH₂ and the H₂ vaporized from the sample. Further heating above 500° C.to 1200° C. resulted in the reaction of the highly reactive Tinanoparticles with the developing carbon atoms being formed from thecarbonization of TPEB during the heat treatment resulting in theformation of TiC nanoparticles embedded in excess carbon formed duringthe simple carbonization process. The refractory TiC ceramic carbonmatrix composite was formed in one step. XRD analysis showed high yieldof TiC nanoparticles and a small amount of crystalline carbon as theproducts formed during the heat treatment.

Example 4

Formation of Refractory TiC Solid Ceramic in One Step by ControlledHeating to 1400° C. Under an Argon Atmosphere—

A sample (67.200 mg) of the precursor composition prepared in Example 1was heated under an argon atmosphere at 5° C./min to 250° C. and held atthis temperature for 2 hr to consolidate to a solid shaped thermosetpolymer. During the heat treatment to 250° C., the sample showed anendothermic transition at about 195° C. attributed to the melting pointof TPEB. The isothermal heat treatment at 250° C. resulted in thereaction of the ethynyl units in the TPEB and conversion to the shapedthermoset polymer. The solid sample composed of TiH₂ and the thermosetpolymer was slowly heated at 1° C./min to 1400° C. and held at thistemperature for 4 hr affording a weight retention of 89.33%. Above 400°C., degradation of the TiH₂ occurred to Ti nanoparticles and H₂ and theH₂ vaporized from the sample. Further heating above 500° C. to 1400° C.resulted in the reaction of the highly reactive Ti nanoparticles withthe developing carbon atoms being formed from the carbonization of TPEBduring the heat treatment resulting in the formation of TiCnanoparticles embedded in excess carbon formed during the simplecarbonization process. The refractory TiC ceramic carbon matrixcomposite was formed in one step. XRD analysis showed high yield of TiCnanoparticles and a small amount of crystalline carbon as the productsformed during the heat treatment.

Example 5

Formation of Refractory TiC Solid Ceramic in One Step by ControlledHeating of 2° C./Min to 1400° C. Under an Argon Atmosphere—

A sample (64.7660 mg) of the precursor composition prepared in Example 1was heated in a TGA chamber under an argon atmosphere at 5° C./min to250° C. and held at this temperature for 2 hr to consolidate to a solidshaped thermoset polymer. During the heat treatment to 250° C., thesample showed an endothermic transition at about 195° C. attributed tothe melting point of TPEB. The isothermal heat treatment at 250° C.resulted in the reaction of the ethynyl units in the TPEB and conversionto the shaped thermoset polymer. The solid sample composed of TiH₂ andthe thermoset polymer was slowly heated at 2° C./min to 1400° C. andheld at this temperature for 4 hr affording a weight retention of89.77%. Above 400° C., degradation of the TiH₂ occurred to Tinanoparticles and H₂ and the H₂ vaporized from the sample. Furtherheating above 500° C. to 1400° C. resulted in the reaction of the highlyreactive Ti nanoparticles with the developing carbon atoms being formedfrom the carbonization of TPEB during the heat treatment resulting inthe formation of TiC nanoparticles embedded in excess carbon formedduring the simple carbonization process. The refractory TiC ceramiccarbon matrix composite was formed in one step. XRD analysis showed highyield of TiC nanoparticles and a small amount of crystalline carbon asthe products formed during the heat treatment.

Example 6

Formation of Stable TiO₂ on Outer Surface as Film from Exposure of TiCSolid Ceramic to Flow of Air—

The TiC carbon composite sample (56.2200 mg) prepared in Example 5 wascooled and further heated in the TGA chamber in a flow of air (100cc/min) at 5° C./min to 1400° C. The sample started to slowly exothermabove 500° C. peaking at about 644° C. with a slight increase in weight.As the heating was continued to 1400° C., an increase in weight of 20%was observed on this small sample attributed to oxidation (white layer)on the outer surface of the sample. XRD analysis confirmed the formationof TiO₂ (white layer) on the outer surface. Below this surface, a blacksurface was intact and attributed to the original TiC-carboncomposition.

Example 7

Controlled Oxidation of TiC Carbon Composite—

The sample (68.2060 mg) formed during the oxidation of Example 6 wascooled and reheated at 10° C./min to 1400° C. under a flow of air (100cc/min). Basically, no change in the weight was observed indicating thatno further oxidation was occurring after the initial oxidation to formthe film (TiO₂) on the outer surface. The TiO₂ was behaving as a barrierprotecting the inner portion of the sample against further oxidation.

Example 8

Melt Formulation of Solid Precursor Composition of TiH₂ and TPEB—

TPEB (0.600 g; 1.255 mmol) was melted at 255° C. in an aluminum planchettreated with a silicone mold release. TiH₂ (1.65 g; 33.1 mmol) was addedto the melt and thoroughly mixed until the mixture thickened(polymerization of the acetylene units to thermoset polymer). Variousprecursor polymeric compositions (TiH₂ and TPEB) can be formulated bythis method by varying the ratio of the two reactants (TPEB and TiH₂).

Example 9

Formation of Refractory TiC Solid Ceramic Carbon Composition in One Stepby Heating at 2° C./Min to 1000° C. Under an Argon Atmosphere—

The thermoset sample (1.98 g) prepared in Example 8 was heated in a tubefurnace at 2° C./min to 1000° C. yielding the solid ceramic materialwith a weight retention of 95%. The sample was characterized by XRD andwas found to form pure nanoparticle sized TiC embedded in an excess ofcarbon as the matrix. The TiC nanoparticle carbon solid composition wasformed in one step and retained its structural integrity.

Example 10

Formation of Refractory TiN Solid Ceramic Carbon Composition in One Stepby Controlled Heating to 1400° C. Under a Nitrogen Atmosphere—

A sample (5.1780 mg) of a precursor composition prepared as in Example 1was weighed into a TGA ceramic pan and heated at 10° C. under a flow(100 cc/min) of nitrogen to 1400° C. yielding a solid material with aweight retention of 89.24%. During the heat treatment, the sample meltedat about 194° C. (endothermic transition; TPEB) and exhibited anexothermic transition peaking at about 292° C. attributed to the cure tosolid thermoset polymer. After the heat treatment at 1400° C., the solidceramic was removed from the TGA pan and characterized by XRD and wasfound to contain TiN nanoparticles embedded or bonded in an excess ofcarbon as the matrix. The TiN carbon solid composition was formed in onestep in the nitrogen atmosphere. In contrast, when the reaction was rununder an argon atmosphere, the TiC nanoparticles (embedded in excesscarbon) were formed from reaction of the Ti nanoparticles with thecarbon atoms during the carbonization process. FIG. 6 shows a typicalXRD of a TiN sample made by the method of this example.

Example 11

Formation of Refractory TiN Solid Ceramic in One Step by ControlledHeating at 2° C./Min to 1400° C. Under a Nitrogen Atmosphere—

A sample (77.4586 mg) of the precursor composition prepared as inExample 1 was heated in a TGA chamber under a nitrogen atmosphere at 5°C./min to 250° C. and held at this temperature for 2 hr to consolidateto a solid shaped thermoset polymer. At this time, the solid polymersample, composed of TPEB and TiH₂, was slowly heated at 2° C./min to1400° C. and held at this temperature for 3 hr affording a solid ceramiccarbon composition with a weight retention of 92.94 wt. During the heattreatment, the sample showed an endothermic transition at about 195° C.attributed to the melting point of TPEB. The isothermal heat treatmentat 250° C. resulted in the reaction of the ethynyl units in the TPEB andconversion to a shaped solid thermoset polymer. Further heating above400° C. resulted in the degradation of the TiH₂ to Ti nanoparticles andH₂, of which the H₂ vaporized from the sample as formed. Further heatingabove 500° C. to 1400° C. resulted in the reaction of the highlyreactive Ti nanoparticles with the developing carbon atoms being formedfrom degradation of TPEB during the carbonization process resulting inthe formation of TiN nanoparticles embedded in excess carbon formed. Therefractory TiN ceramic carbon matrix composition was formed in one step.XRD analysis of the solid ceramic carbon matrix composition showed highyield of nanoparticle TiN nanoparticles and crystalline carbon as theproducts from the heat treatment.

Example 12

Formation of Solid Precursor Composition of TiH₂ and PDEA by MeltMixing—

N,N′-(1,4-phenylenedimethylidyne)-bis-(3-ethynylaniline) (PDEA) (0.516g; 1.394 mmol) was melted at 160° C. in an aluminum planchet treatedwith a silicone mold release. TiH₂ (1.65 g; 33.1 mmol) was added to themelt, thoroughly mixed, and heated under an argon atmosphere until themixture thickened from polymerization of the terminal acetylene units toa thermoset polymer. The solid thermoset polymer composition was heatedat 160° C. for 1 hr was cooled, removed from the mold, and used for theformation of refractory nanoparticle TiC and TiN compositions.

Example 13

Conversion of Solid Precursor Composition TiH₂ and PDEA to RefractoryTiC/TiN Solid Ceramic in One Step by Heating at 10° C./Min to 1000° C.Under an Argon Atmosphere—

A sample (1.896 g) prepared as in Example 12 was heated under anatmosphere of argon in a tube furnace at 2° C./min to 1000° C. yieldingthe solid ceramic material with a weight retention of 95%. The samplewas characterized by XRD and was found to contain both TiC and TiNembedded in an excess of carbon as the matrix. The TiC and TiNnanoparticle carbon solid composition was formed in one step andretained its structural integrity. When another small sample was heatedin a nitrogen atmosphere, only TiN nanoparticles embedded in carbon wereformed.

Example 14

Formulation of Solid Precursor Thermoset Polymeric Composition of TiH₂and Dianilphthalonitrile by Melt Mixing—

Dianilphthalonitrile (0.600 g; 1.56 mmol) was melted at 300° C. in analuminum planchet treated with a silicone mold release. TiH₂(1.66 g;33.2 mmol) and 3 weight % p-BAPS (curing additive) were added,thoroughly mixed, and heated at 300° C. until the mixture thickened frompolymerization of the terminal phthalonitrile units to a thermosetpolymer. Once solidified by heating at 300° C. for 1 hr, the solidpolymeric mass was cooled, removed from the mold, and used for theformation of refractory nanoparticle TiC and TiN nanoparticles embeddedor bonded within the excess carbon that behaves as a matrix material.The ratio of the two reactants can be varied by this described methodand will yield a thermoset polymer with homogeneous distribution of theTiH₂ within the domain of the polymer. The overall physical propertiesof the polymer can be easily varied with varying amounts of thereactants.

Example 15

Conversion of Solid Precursor Thermoset Polymeric Composition of TiH₂and Dianilphthalonitrile to Refractory TiC and TiN Solid Carbon Ceramicin One Step by Heating at 10° C./Min to 1000° C. Under an ArgonAtmosphere—

A polymeric sample (2.068 g) prepared as in Example 14 was heated underan argon atmosphere in a tube furnace at 2° C./min to 1000° C. yieldingthe solid ceramic material with a weight retention of 92.1%. The ceramicsample was characterized by XRD and was found to containnanoparticle-containing TiC and TiN embedded in an excess of carbon asthe matrix. The TiC and TiN carbon solid ceramic composition was formedin one step and retained its structural integrity.

Example 16

Formulation of Solid Precursor Composition of TiH₂ and ResorcinolPhthalonitrile by Melt Mixing—

Resorcinol phthalonitrile (0.500 g; 1.381 mmol) was melted at 300° C. inan aluminum planchet treated with a silicone mold release. TiH₂ (1.65 g;33.1 mmol) and 3 weight % p-BAPS were added, thoroughly mixed, andheated at 300° C. under an argon atmosphere until the mixture thickenedfrom polymerization of the terminal phthalonitrile units to a thermosetpolymer. Once solidified by heating at 300° C. for 1 hr, the solidpolymeric mass was cooled, removed from the mold, and used for theformation of refractory nanoparticle TiC and TiN carbon compositions.

Example 17

Conversion of Solid Precursor Thermoset Polymeric Composition of TiH₂and Resorcinol Phthalonitrile to Refractory TiC and TiN Solid Ceramic inOne Step by Heating at 10° C./Min to 1000° C. Under an Argon Atmosphere—

A polymeric sample (1.978 g) prepared as in Example 16 was heated in atube furnace at 2° C./min to 1000° C. yielding the solid ceramicmaterial with a weight retention of 91.5%. The ceramic sample wascharacterized by XRD and was found to contain nanoparticle-containingTiC and TiN embedded in carbon as the matrix. The TiC and TiN carbonsolid shaped composition was formed in one step and retained itsstructural integrity.

Example 18

Formulation and Formation of Solid Cone-Shaped Thermoset PolymericComposition of TiH₂ and TPEB by Melt Mixing—

TPEB (3.61 g; 7.552 mmol) was melted at 255° C. in an aluminum foil moldthat had been pressed into a conical shape and treated with a siliconemold release. TiH₂ (7.18 g; 143.7 mmol) was added, thoroughly mixed, andheated under an argon atmosphere until the mixture thickened bypolymerization of the acetylene units to a thermoset polymer. Once thecomposition had solidified (30 min), the solid shaped polymeric mass wascooled and removed from the mold. The ratio of the two reactants can beeasily varied by the method described in this Example 18 for formulationto a thermoset polymer. Using the various solid thermoset polymericcomposition containing varying amounts of the two reactants, the overallphysical properties of the corresponding TiC-carbon matrix composition,by heating the polymeric compositions above 500° C. under a flow ofargon, can be readily changed. In addition, the amounts of each reactantcan be changed to afford the formation of just TiC nanoparticles or TiCnanoparticles embedded in varying amounts of carbon.

Example 19

Conversion of Solid Cone-Shaped Thermoset Polymeric Composition of TiH₂and TPEB to Refractory TiC Solid Cone-Shaped Ceramic in One Step byHeating at 10° C./Min to 1000° C. Under an Argon Atmosphere—

A thermoset polymer sample (9.962 g) prepared as in Example 18 washeated in a tube furnace at 2° C./min to 1000° C. yielding the solidceramic material with a weight retention of 91.2%. The ceramic samplewas characterized by XRD and was found to contain TiC nanoparticlesembedded in an excess of carbon as the matrix. The refractory TiCceramic carbon solid composition was formed in one step and retained itsstructural integrity. This example shows that any shaped configurationcontaining refractory metal carbide in carbon as matrix can be formedfrom a refractory metal source that degrades or decomposes to metalnanoparticles that react with the developing carbon atoms of a carbonsource (resin or polymer) during the elevated heat treatment under inertconditions.

Example 20

Formulation of Precursor Composition of ZrH₂ and TPEB—

TPEB (0.0.0974 g; 0.203 mmol) and ZrH₂ (0.500 g; 5.361 mmol) werethoroughly mixed as powders and used as the precursor for the formationof refractory ZrC or ZrN nanoparticles embedded or bonded with theslight excess carbon that behaves as a matrix material. The ratio of thetwo reactants can be varied to form various concentrations of powderedprecursor composition.

Example 21

Formation of Refractory ZrC Solid Ceramic Composition in One Step byHeating at 10° C./Min to 1400° C. Under an Argon Atmosphere—

A sample (20.9090 mg) of the precursor composition prepared in Example20 was weighed into a TGA ceramic pan and heated at 10° C. under a flow(100 cc/min) of argon to 1400° C. yielding a solid material with aweight retention of 94.34%. During the heat treatment, the sample meltedat about 194° C. (endothermic transition; TPEB) and exhibited anexothermic transition peaking at about 292° C. attributed to the cure toa solid thermoset polymer. After cooling from 1400° C. to roomtemperature, the solid ceramic composition was removed from the TGA pan,characterized by XRD and was found to contain nanoparticle sized ZrC inan excess of carbon as the matrix. The shaped solid ceramic refractoryZrC carbon composite was formed in one step and exhibited structuralintegrity. FIG. 7 shows a typical XRD of a ZrC sample made by the methodof this example.

Example 22

Formation of Refractory ZrC Solid Ceramic in One Step by ControlledHeating of 2° C./Min to 1400° C. Under an Argon Atmosphere—

A sample (124.1630 mg) of the powdered composition prepared as inExample 20 was heated in a TGA chamber under an argon atmosphere at 5°C./min to 250° C. and held at this temperature for 2 hr to consolidateto a solid shaped thermoset polymer. During the heat treatment, thesample showed an endothermic transition at about 195° C. attributed tothe melting point of TPEB. The isothermal heat treatment at 250° C.resulted in the reaction of the ethynyl units in the TPEB and conversionto the shaped solid thermoset polymer. The resulting thermoset polymercontained a homogeneous distribution of ZrH₂ embedded in the domain ofthe polymer. Further heating above 500° C. resulted in the degradationof the ZrH₂ to Zr nanoparticles and H₂; the H₂ vaporized from the sampleas formed. Heating from 500° C. to 1400° C. resulted in the reaction ofthe highly reactive Zr nanoparticles with the developing carbon atomsbeing formed from degradation of TPEB during the simple carbonizationprocess resulting in the formation of ZrC nanoparticles embedded inexcess carbon. The solid thermoset polymer sample was slowly heated at2° C./min to 1400° C. and held at this temperature for 4 hr affording aweight retention of 93.77 wt of a solid ceramic solid. The refractoryZrC ceramic carbon matrix composition is formed in one step. XRDanalysis showed high yield of ZrC nanoparticles and a small amount ofcrystalline carbon as the products formed during the heat treatment.

Example 23

Mixing and Conversion of Precursor Compositions of TiH₂/TPEB andZrH₂/TPEB to Refractory TiC and ZrC in Carbon Matrix in One Step byHeating in Argon Atmosphere to 1000° C.—

A sample (30.1234 mg) of TiH₂/TPEB powdered composition prepared as inExample 1 and a sample (55.2685 mg) of ZrH₂/TPEB powdered compositionprepared as in Example 20 were thoroughly mixed and placed in a TGA pan.The resulting mixture was heated at 2° C. under a flow (100 cc/min) ofargon to 1200° C. yielding a solid material with a weight retention of94.34%. During the heat treatment, the sample melted at about 194° C.(endothermic transition; TPEB) and exhibited an exothermic transitionpeaking at about 292° C. attributed to the cure of the TPEB to solidthermoset polymer. After cooling from 1200° C. to room temperature, thesolid ceramic material was removed from the TGA pan, characterized byXRD and was found to contain nanoparticle sized TiC and ZrC in an excessof carbon as the matrix. The shaped solid ceramic refractory TiC and ZrCcarbon composition was formed in one step and exhibited structuralintegrity.

Example 24

Formation of Refractory ZrN Solid Ceramic in One Step by Heating at 10°C./Min to 1400° C. Under an Argon Atmosphere—

A sample (31.51895 mg) of the precursor composition prepared as inExample 20 was weighed into a TGA ceramic pan and heated at 10° C. undera flow (100 cc/min) of nitrogen to 1400° C. yielding a solid materialwith a weight retention of 96.5%. During the heat treatment, the samplemelted at about 194° C. (endothermic transition; TPEB) and exhibited anexothermic transition peaking at about 292° C. attributed to the cure ofTPEB to solid thermoset polymer. After cooling from 1400° C. to roomtemperature, the solid ceramic material was removed from the TGA pan,characterized by XRD, and was found to contain nanoparticle sized ZrNembedded in an excess of carbon as the matrix. The shaped solid ZrNcarbon composite was formed in one step and exhibited structuralintegrity. ZrN was formed rather than ZrC because of the nitrogenatmosphere, which was the source of the nitrogen in the refractory ZrNnanoparticles. FIG. 8 shows a typical XRD of a ZrN sample made by themethod of this example.

Example 25

Melt Formulation of Solid Precursor Thermoset Polymeric Composition ofZrH₂ and TPEB—

TPEB (0.792 g; 1.66 mmol) was melted at 255° C. in an aluminum planchettreated with a silicone mold release. ZrH₂ (3.00 g; 32.2 mmol) was addedto the melt, thoroughly mixed, and heated at 255° C. under an inertatmosphere until the mixture thickened from polymerization of theacetylene units of TPEB to a thermoset polymer. Once solidification (30min) had occurred to a shaped thermoset polymer, the solid polymer masswas cooled and removed from the mold. By the method described, the ratioof the two reactants (TPEB and ZrH₂) can be varied, which will affectthe overall physical properties of the thermoset polymer containing ahomogeneous distribution of ZrH₂ within the domain of the polymericthermoset.

Example 26

Conversion of Solid Precursor Thermoset Polymeric Composition of ZrH₂and TPEB to Refractory ZrC Solid Ceramic in One Step by Heating at 10°C./Min to 1000° C. Under an Argon Atmosphere—

A sample (3.156 g) of solid thermoset composition prepared as in Example25 was placed in a tube furnace and heated under an argon atmosphere at2° C./min to 1000° C. yielding the solid ceramic material with a weightretention of 94%. The sample was characterized by XRD and was found tocontain a homogeneous distribution of ZrC nanoparticles in an excess ofcarbon as the matrix. The ZrC nanoparticle carbon solid composition wasformed in one step and retained its solid structural integrity.

Example 27

Conversion of Solid Precursor Thermoset Polymeric Composition of ZrH₂and TPEB to Refractory ZrN Solid Ceramic in One Step by Heating at 10°C./Min to 1000° C. Under a Nitrogen Atmosphere—

Another polymeric sample (4.523 g) prepared as in Example 25 was placedin a tube furnace and heated under a nitrogen atmosphere at 2° C./min to1000° C. yielding the solid ceramic material with a weight retention of99%. The sample was characterized by XRD and was found to form a ZrNnanoparticle carbon composition. At least the ZrN was present on theouter surfaces in an excess of carbon as the matrix. The ZrNnanoparticle carbon solid composition was formed in one step and thesample retained its solid structural integrity. A large thick samplewould probably contain ZrN on the outer part of the sample and ZrC inthe interior part of the sample.

Example 28

Formulation of Precursor Composition of HfH₂ and TPEB—

TPEB (0.0.0974 g; 0.203 mmol) and HfH₂ (0.500 g; 5.361 mmol) werethoroughly mixed in the powder form and used as the precursor for theformation of shaped solid HfH₂ polymeric compositions.

Example 29

Formulation of Precursor Composition of HfH₂ and TPEB—

TPEB (87 mg; 0.182 mmol) and HfH₂ (1.00 mg; 5.54 mmol) were thoroughlymixed and used as the precursor for the formation of refractorynanoparticle HfC embedded or bonded with the slight excess carbon thatbehaves as a matrix material. The ratio of the two reactants can beeasily varied which will affect the overall physical properties of thecorresponding HfH₂ thermoset polymers, which are readily converted toHfC-carbon matrix compositions by heating the polymeric compositionsabove 500° C. in an argon atmosphere. In addition, the amounts of eachreactant can be changed to afford basically the formation of just HfC inwhich the ratio of Hf atoms to carbon atoms is 1:1.

Example 30

Formation of Refractory HfC Solid Ceramic Composition in One Step byHeating at 10° C./Min to 1400° C. Under an Argon Atmosphere—

A sample (71.8978 mg) of the precursor mixture prepared in Example 28was weighed into a TGA ceramic pan and heated at 10° C. under a flow(100 cc/min) of argon to 1400° C. yielding a solid material with aweight retention of 98.45%. During the heat treatment, the TPEB in theprecursor mixture melted at about 194° C. (endothermic transition; TPEB)and exhibited an exothermic transition peaking at about 292° C.attributed to the cure of TPEB to a solid thermoset polymer. Aftercooling from 1400° C. to room temperature, the solid ceramic materialwas removed from the TGA pan, characterized by XRD and was found tocontain nanoparticle sized HfC in an excess of carbon as the matrix. Theshaped solid ceramic refractory HfC carbon composite was formed in onestep and exhibited structural integrity. FIG. 9 shows a typical XRD of aHfC sample made by the method of this example.

Example 31

Formation of Refractory HfN Solid Ceramic Composition in One Step byHeating at 10° C./Min to 1400° C. Under an Argon Atmosphere—

A sample (75.7452 mg) of the precursor mixture prepared in Example 28was weighed into a TGA ceramic pan and heated at 10° C. under a flow(100 cc/min) of nitrogen to 1400° C. yielding a solid material with aweight retention of 99.34%. During the heat treatment, the TBEB in theprecursor mixture melted at about 194° C. (endothermic transition; TPEB)and exhibited an exothermic transition peaking at about 292° C.attributed to the cure of TPEB to a solid thermoset polymer. Aftercooling from 1400° C. to room temperature, the solid ceramic was removedfrom the TGA pan, characterized by XRD and was found to containnanoparticle sized HfN in an excess of carbon as the matrix. The shapedsolid ceramic refractory HfN carbon composite was formed in one step andexhibited structural integrity.

Example 32

Formation of Refractory HfC Solid Ceramic Composition in One Step byHeating at 10° C./Min to 1400° C. Under an Argon Atmosphere—

A sample (71.8978 mg) of the precursor mixture prepared in Example 29was weighed into a TGA ceramic pan and heated at 5° C. under a flow (100cc/min) of argon to 1400° C. yielding a solid material with a weightretention of 98.89%. After cooling from 1400° C. to room temperature,the solid ceramic material was removed from the TGA pan, characterizedby XRD and was found to contain nanoparticle sized HfC in an excess ofcarbon as the matrix. The shaped solid ceramic refractory HfC carboncomposite was formed in one step and exhibited structural integrity.

Example 33

Formulation of Solid Precursor Composition of Tungsten Powder (˜600-900nm Particle Size) and TPEB by Melt Mixing—

TPEB (0.680 g; 1.422 mmol) was melted at 250° C. in an aluminum planchettreated with a silicone mold release. Tungsten powder (2.00 g; 10.87mmol) was added, thoroughly mixed, and heated at 250° C. until themixture thickened attributed to the polymerization of the acetyleneunits of TPEB to thermoset polymer. On solidification (30 min) of theTPEB to the thermoset polymer, the solid shaped polymer mass was cooledand removed from the mold.

Example 34

Formation of Refractory WC Solid Ceramic in One Step by Heating at 10°C./Min to 1000° C. Under an Argon Atmosphere—

A sample (2.542 g) of the polymeric composition prepared in Example 33was heated in a tube furnace at 2° C./min to 1000° C. yielding the solidceramic material with a weight retention of 95%. The sample wascharacterized by XRD and was found to contain WC in a large excess ofcarbon as the matrix along with some unreacted tungsten. The WC carbonsolid composite was formed in one step. Nanoparticle-sized tungsten orsmall-sized tungsten powder would be expected to increase the yield ofWC and potentially eliminate the presence of unreacted tungsten. Heatingof the sample at a higher temperature (1200° C.) reduced the amount ofunreacted tungsten and increased the amount of WC present in the sample.

Example 35

Formulation of Precursor Composition of TiH₂ and TPEB with Excess CarbonSource (TPEB)—

TPEB (2.10 g; 4.39 mmol) and TiH₂ (4.95 g; 99.1 mmol) were thoroughlymixed in the powder form and used as the precursor for the formation ofrefractory nanoparticle TiC in a carbon matrix carbon fiber composite.

Example 36

Formulation of TiH₂ Carbon Fiber Polymeric Composite—

Into a 0.5 inch diameter mold formed from aluminum foil was placed theprecursor composition (1.7541 g of the TPEB and TiH₂ mixture) preparedin Example 35. The mixture was heated to 220° C. (melt) and choppedcarbon fibers were added and mixed into the composition. The resultingcarbon fiber-precursor composition was heated under a flow of argon at250° C. for 1 hr resulting in solidification to a shaped carbonfiber-containing polymeric thermoset.

Example 37

Conversion of the TiH₂ Carbon Fiber Polymeric Composite to TiC CarbonFiber Ceramic Composite—

The solid shaped carbon fiber polymeric composite prepared in Example 36with a homogeneous distribution of the TiH₂ was removed from the mold,placed in an oven, and heated under a flow of argon at 3° C./min to1000° C. and held at the temperature for 2 hr. The resultingceramic-carbon reinforced composite was cooled at 3° C./min back to roomtemperature. The solid composite sample was characterized by XRD andfound to contain refractory TiC nanoparticles embedded in carbon matrixand carbon fibers.

Example 38

Formation of Refractory ZrH₂ Carbon Fiber Polymeric Composite—

Into a 0.5 inch diameter mold fabricated from aluminum foil was placed aprecursor composition (1.9545 g of the TPEB and ZrH₂ mixture) preparedas in Example 20. The composition was heated to 220° C. (melt) andchopped carbon fibers were added and mixed into the liquid composition.The resulting carbon fiber-precursor composition was heated under a flowof argon at 250° C. for 1 hr resulting in solidification to a shapedcarbon fiber-containing polymeric thermoset. The solid shaped carbonfiber polymeric composite with a homogeneous distribution of the ZrH₂was removed from the mold.

Example 39

Conversion of the ZrH₂ Carbon Fiber Polymeric Composite to ZrC CarbonFiber Ceramic Composite—

The solid shaped carbon fiber polymeric composite prepared in Example 38was placed in an oven and heated under a flow of argon at 3° C./min to1200° C. and held at the temperature for 2 hr. The resultingceramic-carbon fiber reinforced composite was cooled at 3° C./min backto room temperature. The solid ceramic-carbon fiber composite sample wascharacterized by XRD and found to contain refractory ZrC nanoparticlesembedded in carbon matrix and carbon fibers.

Example 40

Formation of Refractory HfH₂ Carbon Fiber Polymeric Composite—

Into a 0.5 inch diameter mold fabricated from aluminum foil was placed aprecursor composition (2.5564 g of the TPEB and HfH₂ mixture) preparedas in Example 29. The composition was heated to 220° C. (melt) andchopped carbon fibers were added and mixed into the liquid composition.The resulting carbon fiber-precursor composition was heated under a flowof argon at 250° C. for 1 hr resulting in solidification to a shapedcarbon fiber-containing polymeric thermoset. The solid shaped carbonfiber polymeric composite with a homogeneous distribution of the HfH₂was removed from the mold.

Example 41

Conversion of the HfH₂ Carbon Fiber Polymeric Composite to HfC CarbonFiber Ceramic Composite—

The solid shaped carbon fiber polymeric composite prepared in Example 40was placed in an oven and heated under a flow of argon at 3° C./min to1200° C. and held at the temperature for 4 hr. The resultingceramic-carbon fiber reinforced composite was cooled at 3° C./min backto room temperature. The solid ceramic-carbon fiber composite sample wascharacterized by XRD and found to contain refractory HfC nanoparticlesembedded in carbon matrix and carbon fibers.

Example 42

Formulation of Precursor Composition of Tantalum Powder (9-12 MicronParticle Size) and TPEB with Excess Carbon Source (TPEB)—

TPEB (0.340 g; 0.711 mmol) and tantalum powder (1.00 g; 5.53 mmol) werethoroughly mixed and used as the precursor composition for the formationof refractory nanoparticle TaC embedded or bonded with the excess carbonthat behaves as a matrix material.

Example 43

Conversion of Precursor Composition of Tantalum Powder (9-12 MicronParticle Size) and TPEB by Heating at 1200° C. for 6 Hr Under Flow ofArgon—

A sample (0.7567 g) of the precursor composition prepared in Example 42was heated at 3° C./min under a flow of argon to 1200° C. and held atthis temperature for 6 hr. The solid sample was cooled to roomtemperature. The solid ceramic sample was characterized by XRD and foundto contain refractory TaC, carbon, and unreacted Ta.

Example 44

Formulation of Prepolymer Composition of TPEB—

TPEB (7.00 g; 14.6 mmol) was placed in an aluminum planchet and heatedat 250° C. for 30 minutes or until the mixture was viscous to stir witha metal spatula. The mixture was cooled, broken into small pieces, andball milled for 2 minutes resulting in a fine black powder.

Example 45

Formulation of Precursor Composition of TiH₂ and TPEB Prepolymer andFormation of Shaped Pellet—

TPEB prepolymer form Example 44 (0.300 g; 0.627 mmol) and TiH₂ (0.825 g;16.5 mmol) were ball milled for 5 minutes resulting in a deep red-blackfine powder. The powder was placed in a 13 mm pellet press and pressedto 10,000 pounds for 1 minute.

Example 46

Conversion of Precursor Composition of TiH₂ and TPEB Prepolymer to SolidShaped Thermoset—

The pellet from Example 45 was placed in a furnace, heated at 20° C./minunder an argon atmosphere to 210° C., and held at this temperature for10 hr (overnight) resulting in the formation of a tough shaped polymericthermoset solid. The TiH₂ was homogeneously dispersed in the solidthermoset.

Example 47

Conversion of Precursor Composition of TiH₂ and TPEB Prepolymer to SolidShaped Thermoset—

Another pellet prepared as in Example 45 was placed in a furnace, heatedat 20° C./min under an argon atmosphere to 250° C., and held at thistemperature for 2 hr resulting in the formation of a tough shapedpolymeric thermoset solid.

Example 48

Formation of Refractory TiC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The shaped polymeric thermoset solid (1.12 g) from Example 46 was placedin a 3″ tube furnace, heated at 2° C./min under a flow (100 cc/min) ofargon to 1600° C., and held at 1600° C. for 2 hr yielding a solid denseceramic with weight retention of 92.1%. The solid ceramic was removedfrom the furnace, characterized by XRD, and found to form nanoparticlesized TiC in an excess of carbon as the matrix. The TiC carbon solidcomposition was formed in one step and exhibited great structuralintegrity, hardness, and toughness. FIG. 10 shows a typical XRD of a TiCsample made by the method of this example.

Example 49

Heat Treatment of Refractory TiC Solid Ceramic by Heating to 1900° C.Under Vacuum—

The 1600° C. treated ceramic pellet (0.839 g) from Example 48 was placedin a graphitic furnace, heated at 10° C./min under a vacuum (10⁻⁴) to1900° C., and held at 1900° C. for 2 hr yielding a solid dense ceramicwith a weight retention of 95.8%. Upon cooling, the solid ceramic wasremoved from the furnace, characterized by XRD, and found to form largernanoparticle sized TiC in an excess of carbon as the matrix. FIG. 11shows a typical SEM of a TiC sample made by the method of this example.

Example 50

Formulation of Precursor Composition of TiH₂ and TPEB Prepolymer,Formation of Shaped Pellet, and Direct Conversion to Refractory TiCSolid Ceramic Carbon Composition in One Step—

TPEB prepolymer (0.305 g, 0.627 mmol) prepared as in Example 44 and TiH₂(0.828 g; 16.5 mmol) were ball milled for 5 minutes resulting in a deepred-black fine powder. The powder was placed in a 13 mm pellet press andpressed to 10,000 pounds for 1 minute. The pellet was then placed in afurnace, heated at 20° C./min under an argon atmosphere to 250° C., andheld at this temperature for 30 minutes followed by heating at 2° C./minunder a flow (100 cc/min) of argon to 1200° C. and holding at 1200° C.for 3 hr yielding a solid dense ceramic with weight retention of 94.8%.Upon cooling, the solid ceramic was removed from the furnace,characterized by XRD, and found to form nanoparticle sized TiC in anexcess of carbon as the matrix. The TiC carbon solid composition wasformed in one step and exhibited great structural integrity, hardness,and toughness.

Example 51

Formulation of Precursor Composition of Tungsten Powder and TPEBPrepolymer and Pellet Formation—

TPEB prepolymer from Example 44 (0.150 g; 0.314 mmol) and tungstenpowder (1.95 g; 10.6 mmol) were ball milled for 5 minutes resulting in adeep red-black fine powder. The powder was placed in a 13 mm pelletpress and pressed to 10,000 pounds for 10 sec.

Example 52

Conversion of Precursor Composition of Tungsten Powder and TPEBPrepolymer to Solid Shaped Thermoset—

The pellet from Example 51 was placed in a furnace, heated at 20° C./minunder an argon atmosphere to 225° C., and held at this temperature for10 hr (overnight) resulting in the formation of a tough shaped polymericsolid. The tungsten powder was homogeneous dispersed in the solidthermoset.

Example 53

Formation of Refractory WC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The cured thermoset pellet (2.03 g) from Example 52 was placed in a 3″tube furnace, heated at 2° C./min under a flow (100 cc/min) of argon to1600° C., and held at 1600° C. for 2 hr yielding a solid dense ceramicwith weight retention of 96.25%. Upon cooling, the solid ceramic wasremoved from the furnace, characterized by XRD, and found to formnanoparticle sized pure WC in an excess of carbon as the matrix. All ofthe tungsten had reacted. The WC carbon solid composition was formed inone step and exhibited structural integrity, hardness, and toughness.FIG. 12 shows a typical XRD of a WC sample made by the method of thisexample. FIG. 13 shows a typical SEM of a WC sample made by the methodof this example.

Example 54

Heat Treatment of Refractory WC Solid Ceramic to 1900° C. Under Vacuum—

The 1600° C. treated solid ceramic pellet (1.95 g) from Example 53 wasplaced in a graphitic furnace, heated at 10° C./min under a vacuum(10⁻⁴) to 1900° C., and held at 1900° C. for 2 hr yielding a weightretention of 99.7%. Upon cooling, the solid ceramic was removed from thefurnace, characterized by XRD, and found to form larger nanoparticlesized WC in an excess of carbon as the matrix relative to the heattreatment to 1600° C. as formed in Example 53. The WC carbon solid stillexhibited great structural integrity, hardness, and retained toughness.

Example 55

Formulation of Precursor Composition of HfH₂ and TPEB Prepolymer—

TPEB prepolymer from Example 44 (0.217 g; 0.454 mmol) and hafniumhydride (2.49 g; 13.8 mmol) were ball milled for 5 minutes resulting ina deep red-black fine powder. The powder was placed in a 13 mm pelletpress and pressed to 10,000 pounds for 10 sec.

Example 56

Conversion of Precursor Composition of HfH₂ and TPEB Prepolymer to SolidShaped Thermoset—

The pellet from Example 55 was placed in a furnace, heated at 20° C./minunder an argon atmosphere to 225° C., and held at this temperature for10 hr (overnight) resulting in the formation of a tough shaped polymericsolid. The hafnium hydride powder was homogeneous dispersed in the solidthermoset.

Example 57

Formation of Refractory HfC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The cured thermoset pellet (2.68 g) from Example 56 was placed in a 3″tube furnace, heated at 2° C. min under a flow (100 cc/min) of argon to1600° C., and held at 1600° C. for 2 hr yielding a solid dense ceramicwith weight retention of 98.5%. Upon cooling, the solid ceramic wasremoved from the furnace, characterized by XRD, and found to formnanoparticle sized pure HfC in an excess of carbon as the matrix. TheHfC carbon solid composition was formed in one step and exhibitedstructural integrity, hardness, and toughness.

Example 58

Heat Treatment of Refractory HfC Solid Ceramic by Heating to and at1900° C. Under Vacuum—

The 1600° C. treated HfC-carbon composition/pellet (1.95 g) from Example57 was placed in a graphitic furnace, heated at 10° C./min under avacuum (10⁻⁴) to 1900° C., and held at 1900° C. for 2 hr yielding asolid dense ceramic with a weight retention of 96.6%. Upon cooling, thesolid ceramic was removed from the furnace, characterized by XRD, andfound to form larger nanoparticle sized HfC in an excess of carbon asthe matrix. The HfC carbon solid exhibited great structural integrity,hardness, and toughness.

Example 59

Formulation of Precursor Composition of ZrH₂ and TPEB Prepolymer—

TPEB prepolymer from Example 44 (0.132 g; 0.276 mmol) and zirconiumhydride (0.500 g; 5.36 mmol) were ball milled for 5 minutes resulting ina deep red-black fine powder. The powder was placed in a 13 mm pelletpress and pressed to 8,000 pounds for 10 sec.

Example 60

Conversion of Precursor Composition of ZrH₂ and TPEB Prepolymer to SolidShaped Thermoset—

The pellet from Example 59 was placed in a furnace, heated at 20° C./minunder an argon atmosphere to 210° C., and held at this temperature for10 hr (overnight) resulting in the formation of a tough shaped polymericsolid. The zirconium hydride powder was homogeneously dispersed in thesolid thermoset.

Example 61

Formation of Refractory ZrC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The cured thermoset pellet (0.630 g) from Example 60 was placed in a 3″tube furnace, heated at 2° C./min under a flow (100 cc/min) of argon to1600° C., and held at 1600° C. for 2 hr yielding a solid dense ceramicwith weight retention of 93.5%. Upon cooling, the solid ceramic wasremoved from the furnace, characterized by XRD, and found to formnanoparticle sized pure ZrC in an excess of carbon as the matrix. TheZrC carbon solid composition was formed in one step and exhibitedstructural integrity, hardness, and toughness.

Example 62

Heat Treatment of Refractory ZrC Solid Ceramic by Heating to 1900° C.Under Vacuum—

The 1600° C. treated ceramic pellet (0.589 g) from Example 61 was placedin a graphitic furnace and heated at 10° C./min under a vacuum (10⁻⁴) to1900° C. for 2 hr yielding a solid dense ceramic with a weight retentionof 96.9%. The solid ceramic was removed from the furnace, characterizedby XRD, and found to form larger nanoparticle sized ZrC in an excess ofcarbon as the matrix. The ZrC carbon solid exhibited great structuralintegrity, hardness, and toughness.

Example 63

Formulation of Precursor Composition of TiH₂ and TPEB PrepolymerContaining Chopped Fibers—

TPEB prepolymer from Example 44 (3.825 g; 8.00 mmol) and TiH₂ (10.52 g;211 mmol) were ball milled for 5 minutes resulting in a deep red-blackfine powder. Chopped fibers (1.00 g, ¼″ length) were added and the solidmixture was placed in 100 mL of acetone and stirred for 6 hr. Thesolvent was removed and the solid mixture was placed in a 2½″ pellet dieand pressed to 10,000 pounds for 1 minute.

Example 64

Conversion of Precursor Composition of TiH₂ and TPEB PrepolymerContaining Chopped Fibers to Thermoset—

The 2½″ pellet from Example 63 was placed in a furnace, heated at 20°C./min under an argon atmosphere to 210° C., and held at thistemperature for 10 hr (overnight) resulting in the formation of a toughshaped polymeric carbon fiber reinforced thermoset solid. The titaniumhydride powder was homogeneous dispersed in the solid thermoset-carbonfiber composite.

Example 65

Formation of Refractory Carbon Fiber Reinforced TiC Solid Ceramic in OneStep by Heating at 10° C./Min to 1600° C. Under an Argon Atmosphere—

The carbon fiber-containing shaped polymeric thermoset pellet (14.9 g)from Example 64 was placed in a 3″ tube furnace and heated at 2° C./minunder a flow (100 cc/min) of argon to 1600° C. yielding a solid densecarbon fiber reinforced ceramic with weight retention of 96.1%. Uponcooling, the solid carbon fiber reinforced ceramic was removed from thefurnace, characterized by XRD, and found to form nanoparticle sized TiCin the carbon-carbon fiber composite. The TiC carbon-carbon fiber solidcomposition exhibited great structural integrity with the inclusion ofthe fiber reinforcement.

Example 66

Formulation of Precursor Composition of ZrH₂ and TPEB PrepolymerContaining Chopped Fibers—

TPEB prepolymer from Example 44 (2.64 g; 5.52 mmol) and ZrH₂ (10.00 g;107 mmol) were ball milled for 5 minutes resulting in a deep red-blackfine powder. Chopped fibers (0.50 g, ¼″ length) were added and the solidmixture was placed in 100 mL of acetone and stirred for 4 hr. Thesolvent was removed and the solid mixture was placed in a 2½″ pellet dieand pressed to 10,000 pounds for 1 minute.

Example 67

Conversion of Precursor Composition of ZrH₂ and TPEB PrepolymerContaining Chopped Fibers to Thermoset—

The 2½″ pellet from Example 66 was placed in a furnace, heated at 20°C./min under an argon atmosphere to 210° C. and held at this temperaturefor 10 hr (overnight) resulting in the formation of a tough shapedcarbon fiber reinforced polymeric solid. The zirconium hydride powderwas homogeneous dispersed in the solid thermoset-carbon fiber composite.

Example 68

Formation of Refractory ZrC Solid Carbon Fiber Reinforced Ceramic in OneStep by Heating at 10° C./Min to 1600° C. Under an Argon Atmosphere—

The carbon fiber-containing shaped polymeric thermoset pellet (12.48 g)from Example 67 was placed in a 3″ tube furnace and heated at 2° C./minunder a flow (100 cc/min) of argon to 1600° C. yielding a solid densecarbon fiber reinforced ceramic with weight retention of 96.7%. Thesolid carbon fiber reinforced ceramic was removed from the furnace,characterized by XRD, and found to form nanoparticle sized ZrC in thecarbon-carbon fiber composite. The ZrC carbon-carbon fiber solidcomposition exhibited great structural integrity with the inclusion ofthe fiber reinforcement.

Example 69

Formulation of Precursor Composition of Tungsten Powder and TPEBPrepolymer Containing Chopped Fibers—

TPEB prepolymer from Example 44 (1.5 g; 3.14 mmol) and tungsten powder(19.5 g; 106 mmol) were ball milled for 5 minutes resulting in a deepred-black fine powder. Chopped fibers (1.50 g, ¼″ length) were added andthe solid mixture was placed in 100 mL of acetone and stirred for 6 hr.The solvent was removed and the solid mixture was placed in a 2½″ pelletdie and pressed to 12,000 pounds for 1 minute.

Example 70

Conversion of Precursor Composition of Tungsten Powder and TPEBPrepolymer Containing Chopped Fibers to Thermoset—

The 2½″ pellet from Example 69 was placed in a furnace, heated at 20°C./min under an argon atmosphere to 210° C., and held at thistemperature for 10 hr (overnight) resulting in the formation of a toughshaped carbon fiber reinforced polymeric solid. The tungsten powder washomogeneous dispersed in the solid thermoset-carbon fiber composite.

Example 71

Formation of Refractory WC Solid Carbon Fiber Reinforced Ceramic in OneStep by Heating at 10° C./Min to 1600° C. Under an Argon Atmosphere—

The carbon fiber-containing shaped polymeric thermoset pellet (21.15 g)from Example 70 was placed in a 3″ tube furnace and heated at 2° C./minunder a flow (100 cc/min) of argon to 1600° C. yielding a solid densecarbon fiber reinforced ceramic with weight retention of 98.1%. Thesolid carbon fiber reinforced ceramic was removed from the furnace,characterized by XRD, and found to form nanoparticle sized WC in thecarbon-carbon fiber composite. The WC carbon-carbon fiber solidcomposition exhibited great structural integrity with the inclusion ofthe fiber reinforcement.

Example 72

Formulation of Precursor Composition of TiH₂ and TPEB Prepolymer at a1C:1Ti Atom Ratio and Formation of Shaped Pellet—

TPEB prepolymer form Example 44 (0.100 g; 0.209 mmol) and TiH₂ (0.398 g;7.94 mmol) were finely ground with a mortar and pestle. The powder wasplaced in an IR pellet press maker from Harrick Scientific Products andwas pressed to form a thin pellet under vacuum.

Example 73 (Prophetic)

Conversion of Precursor Composition of TiH₂ and TPEB Prepolymer (1C:1Ti)to Solid Shaped Thermoset—

The pellet from Example 72 contained in the IR pellet press maker istreated to 300° C. in a vacuum oven for 2 hr to complete crosslinking ofthe prepolymer and released from the IR pellet press maker. Thecrosslinked pellet is further gradually thermally treated under vacuumto 500° C. and it held at this temperature for 2 hr.

Example 74 (Prophetic)

Formation of Refractory TiC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The shaped polymeric thermoset solid from Example 73 is placed in a 3″tube furnace, heated at 2° C./min under a flow (100 cc/min) of argon to1600° C., and held at 1600° C. for 2 hr. The solid ceramic is removedfrom the furnace and characterized by XRD, and is expected to formnanoparticle sized TiC in an excess of carbon as the matrix.

Example 75

Formulation of Precursor Composition of TiH₂ and TPEB Prepolymer at a1C:0.9Ti Atom Ratio and Formation of Shaped Pellet—

TPEB prepolymer form Example 44 (0.100 g; 0.209 mmol) and TiH₂ (0.359 g;7.15 mmol) were finely ground with a mortar and pestle. The powder wasplaced in an IR pellet press maker and was pressed to form a thin pelletunder vacuum.

Example 76 (Prophetic)

Conversion of Precursor Composition of TiH₂ and TPEB Prepolymer(1C:0.9Ti) to Solid Shaped Thermoset—

The pellet from Example 75 contained in the IR pellet press maker istreated to 300° C. in a vacuum oven for 2 hr to complete crosslinking ofthe prepolymer and released from the IR pellet press maker. Thecrosslinked pellet is further gradually thermally treated under vacuumto 500° C. and it was held at this temperature for 2 hr.

Example 77 (Prophetic)

Formation of Refractory TiC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The shaped polymeric thermoset solid from Example 76 is placed in a 3″tube furnace, heated at 2° C./min under a flow (100 cc/min) of argon to1600° C., and held at 1600° C. for 2 hr. The solid ceramic is removedfrom the furnace, characterized by XRD, and is expected to formnanoparticle sized TiC in an excess of carbon as the matrix.

Example 78

Formulation of Precursor Composition of TiH₂ and TPEB Prepolymer at a1C:0.8Ti Atom Ratio and Formation of Shaped Pellet—

TPEB prepolymer form Example 44 (0.100 g; 0.209 mmol) and TiH₂ (0.319 g;6.35 mmol) were finely ground with a mortar and pestle. The powder wasplaced in an IR pellet press maker and was pressed to form a thin pelletunder vacuum.

Example 79 (Prophetic)

Conversion of Precursor Composition of TiH₂ and TPEB Prepolymer(1C:0.8Ti) to Solid Shaped Thermoset—

The pellet from Example 78 contained in the IR pellet press maker istreated to 300° C. in a vacuum oven for 2 hr to complete crosslinking ofthe prepolymer and released from the IR pellet press maker. Thecrosslinked pellet is further gradually thermally treated under vacuumto 500° C. and held at this temperature for 2 hr.

Example 80 (Prophetic)

Formation of Refractory TiC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The shaped polymeric thermoset solid from Example 79 is placed in a 3″tube furnace, heated at 2° C./min under a flow (100 cc/min) of argon to1600° C., and held at 1600° C. for 2 hr. The solid ceramic is removedfrom the furnace, characterized by XRD, and is expected to formnanoparticle sized TiC in an excess of carbon as the matrix.

Example 81

Formulation of Precursor Composition of TiH₂ and TPEB Prepolymer at a1C:0.7Ti Atom Ratio and Formation of Shaped Pellet—

TPEB prepolymer form Example 44 (0.100 g; 0.209 mmol) and TiH₂ (0.279 g;5.56 mmol) were finely ground with a mortar and pestle. The powder wasplaced in an IR pellet press maker and was pressed to form a thin pelletunder vacuum.

Example 82 (Prophetic)

Conversion of Precursor Composition of TiH₂ and TPEB Prepolymer(1C:0.7Ti) to Solid Shaped Thermoset—

The pellet from Example 81 contained in the IR pellet press maker istreated to 300° C. in a vacuum oven for 2 hr to complete crosslinking ofthe prepolymer and released from the IR pellet press maker. Thecrosslinked pellet is further gradually thermally treated under vacuumto 500° C. and held at this temperature for 2 hr.

Example 83 (Prophetic)

Formation of Refractory TiC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The shaped polymeric thermoset solid from Example 83 is placed in a 3″tube furnace, heated at 2° C./min under a flow (100 cc/min) of argon to1600° C., and held at 1600° C. for 2 hr. The solid ceramic is removedfrom the furnace, characterized by XRD, and is expected to formnanoparticle sized TiC in an excess of carbon as the matrix.

Example 84

Formulation of Precursor Composition of TiH₂ and TPEB Prepolymer at a1C:0.6Ti Atom Ratio and Formation of Shaped Pellet—

TPEB prepolymer form Example 44 (0.100 g; 0.209 mmol) and TiH₂ (0.239 g;4.76 mmol) were finely ground with a mortar and pestle. The powder wasplaced in an IR pellet press maker and was pressed to form a thin pelletunder vacuum.

Example 85 (prophetic)

Conversion of Precursor Composition of TiH₂ and TPEB Prepolymer(1C:0.6Ti) to Solid Shaped Thermoset—

The pellet from Example 84 contained in the IR pellet press maker istreated to 300° C. in a vacuum oven for 2 hr to complete crosslinking ofthe prepolymer and released from the IR pellet press maker. Thecrosslinked pellet is further gradually thermally treated under vacuumto 500° C. and it was held at this temperature for 2 hr.

Example 86 (Prophetic)

Formation of Refractory TiC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The shaped polymeric thermoset solid from Example 85 is placed in a 3″tube furnace, heated at 2° C./min under a flow (100 cc/min) of argon to1600° C., and held at 1600° C. for 2 hr. The solid ceramic is removedfrom the furnace, characterized by XRD, and is expected to formnanoparticle sized TiC in an excess of carbon as the matrix.

Example 87

Formulation of Precursor Composition of TiH₂ and TPEB Prepolymer at a1C:0.5Ti Atom Ratio and Formation of Shaped Pellet—

TPEB prepolymer form Example 44 (0.100 g; 0.209 mmol) and TiH₂ (0.199 g;3.97 mmol) were finely ground with a mortar and pestle. The powder wasplaced in an IR pellet press maker and was pressed to form a thin pelletunder vacuum.

Example 88 (Prophetic)

Conversion of Precursor Composition of TiH₂ and TPEB Prepolymer(1C:0.5Ti) to Solid Shaped Thermoset—

The pellet from Example 87 contained in the IR pellet press maker istreated to 300° C. in a vacuum oven for 2 hr to complete crosslinking ofthe prepolymer and released from the IR pellet press maker. Thecrosslinked pellet is further gradually thermally treated under vacuumto 500° C. and it was held at this temperature for 2 hr.

Example 89 (Prophetic)

Formation of Refractory TiC Solid Ceramic in One Step by Heating at 10°C./Min to 1600° C. Under an Argon Atmosphere—

The shaped polymeric thermoset solid from Example 88 is placed in a 3″tube furnace, heated at 2° C./min under a flow (100 cc/min) of argon to1600° C., and held at 1600° C. for 2 hr. The solid ceramic is removedfrom the furnace, characterized by XRD, and is expected to formnanoparticle sized TiC in an excess of carbon as the matrix.

Obviously, many modifications and variations are possible in light ofthe above teachings. It is therefore to be understood that the claimedsubject matter may be practiced otherwise than as specificallydescribed. Any reference to claim elements in the singular, e.g., usingthe articles “a,” “an,” or “the” is not construed as limiting theelement to the singular.

What is claimed is:
 1. A composition comprising: a refractory-metalhydride; and an organic compound having a char yield of at least 60% byweight.
 2. The composition of claim 1, wherein the refractory-metalhydride is titanium hydride, zirconium hydride, hafnium hydride,tungsten hydride, niobium hydride, molybdenum hydride, chromium hydride,tantalum hydride, or vanadium hydride.
 3. The composition of claim 1,wherein the organic compound: contains only carbon and hydrogen;contains aromatic and acetylene groups; contains only carbon, hydrogen,and nitrogen or oxygen; contains no oxygen; or contains a heteroatomother than oxygen.
 4. The composition of claim 1, wherein the organiccompound is 1,2,4,5-tetrakis(phenylethynyl)benzene or a prepolymerthereof, N, N′-(1,4-phenylenedimethylidyne)-bis-(3-ethynylaniline),dianilphthalonitrile, or resorcinol phthalonitrile.
 5. The compositionof claim 1, wherein the composition comprises a material selected fromthe group consisting of, carbon fibers, ceramic fibers, and metalfibers.
 6. A composition comprising: a refractory-metal hydride; and athermoset made from an organic compound having a char yield of at least60% by weight.
 7. The composition of claim 6, wherein therefractory-metal hydride is titanium hydride, zirconium hydride, hafniumhydride, tungsten hydride, niobium hydride, molybdenum hydride, chromiumhydride, tantalum hydride, or vanadium hydride.
 8. The composition ofclaim 6, wherein the organic compound: contains only carbon andhydrogen; contains aromatic and acetylene groups; contains only carbon,hydrogen, and nitrogen or oxygen; contains no oxygen; or contains aheteroatom other than oxygen.
 9. The composition of claim 6, wherein theorganic compound is 1,2,4,5-tetrakis(phenylethynyl)benzene or aprepolymer thereof, N,N′-(1,4-phenylenedimethylidyne)-bis-(3-ethynylaniline),dianilphthalonitrile, or resorcinol phthalonitrile.
 10. The compositionof claim 6, wherein the composition comprises a material selected fromthe group consisting of, carbon fibers, ceramic fibers, and metalfibers.
 11. A composition comprising: nanoparticles or particles of arefractory metal; and a thermoset made from an organic compound having achar yield of at least 60% by weight; wherein the composition comprisesat least 10% by weight of the nanoparticles or particles of therefractory metal.
 12. The composition of claim 11, wherein therefractory metal is titanium.
 13. The composition of claim 11, whereinthe refractory metal is selected from the group consisting of titanium,zirconium, hafnium, tungsten, niobium, molybdenum, chromium, tantalum,and vanadium.
 14. The composition of claim 11, wherein the organiccompound: contains only carbon and hydrogen; contains aromatic andacetylene groups; contains only carbon, hydrogen, and nitrogen oroxygen; contains no oxygen; or contains a heteroatom other than oxygen.15. The composition of claim 11, wherein the organic compound is1,2,4,5-tetrakis(phenylethynyl)benzene or a prepolymer thereof, N,N′-(1,4-phenylenedimethylidyne)-bis-(3-ethynylaniline),dianilphthalonitrile, or resorcinol phthalonitrile.
 16. The compositionof claim 11, wherein the composition comprises a material selected fromthe group consisting of, carbon fibers, ceramic fibers, and metalfibers.
 17. The composition of claim 11, wherein the compositioncomprises at least 70% by weight of the nanoparticles or particles ofthe refractory metal.
 18. A composition comprising: nanoparticles orparticles of a refractory metal; and an organic compound having a charyield of at least 60% by weight; wherein the composition comprises atleast 10% by weight of the nanoparticles or particles of the refractorymetal.
 19. The composition of claim 18, wherein the refractory metal istitanium.
 20. The composition of claim 18, wherein the refractory metalis selected from the group consisting of titanium, zirconium, hafnium,tungsten, niobium, molybdenum, chromium, tantalum, and vanadium.
 21. Thecomposition of claim 18, wherein the metal component is selected fromthe group consisting of particles of the refractory metal, tungstenpowder, and tantalum powder.
 22. The composition of claim 18, whereinthe organic compound: contains only carbon and hydrogen; containsaromatic and acetylene groups; contains only carbon, hydrogen, andnitrogen or oxygen; contains no oxygen; or contains a heteroatom otherthan oxygen.
 23. The composition of claim 18, wherein the organiccompound is 1,2,4,5-tetrakis(phenylethynyl)benzene or a prepolymerthereof, N, N′-(1,4-phenylenedimethylidyne)-bis-(3-ethynylaniline),dianilphthalonitrile, or resorcinol phthalonitrile.
 24. The compositionof claim 18, wherein the composition comprises a material selected fromthe group consisting of, carbon fibers, ceramic fibers, and metalfibers.
 25. The composition of claim 18, wherein the compositioncomprises at least 70% by weight of the nanoparticles or particles ofthe refractory metal.